212 Information Letters


File Name
Date Posted
Description
  IL_212-14-68.pdf 25-Jul-14 GLOBAL ALTERNATE METHOD OF COMPLIANCE (AMOC) FOR AIRWORTHINESS DIRECTIVE (AD) 2014-12-04.
  IL_212-14-67.pdf 10-Jul-14 MAIN ROTOR GRIPS 204-011-121-009/-121 LIFE LIMITATION PER FAA AD 2014-12-04.
  IL_212-13-66.pdf 07-Jan-13 REMOVAL OF ZINC CHROMATE PRIMER STRIPES AS AN OVERHEAT CONDITION INDICATION.
  IL_212-12-65.pdf 10-Sep-12 ENGINE NII (NF) GOVERNOR POSSIBLE ANOMALY
  IL_212-11-INDEX.pdf 01-Mar-12 INFORMATION LETTER INDEX
  IL_212-11-64.pdf 26-Apr-11 FUEL FILTER LIGHT FLICKERING
  IL_212-04-55_Rev_B.pdf 14-Sep-10 BLR FASTFIN AND STRAKE INSTALLATION ON ALL BELL 204,205, 205B, AND 212 MODEL HELICOPTERS.
  IL212-10-63_Rev_A.pdf 09-Apr-10 DERIVED EMPTY WEIGHT CLARIFICATIONS.
  IL_212-08-62_Rev_A.pdf 23-Jul-08 GRIP ASSEMBLY P/N 204-011-121-125, INTRODUCTION OF
  IL_212-05-56_Rev_A.pdf 13-Dec-06 CHANGE TO RECOMMENDED INTERVALS FOR PLANNED MAINTENANCE OF BREEZE-EASTERN RESCUE HOISTS AND CARGO WINCHES
  IL_212-06-61.pdf 22-Jun-06 MODEL 212 SHEETMETAL ENGINE DECK
  IL_212-06-60.pdf 19-Jan-06 ENGINE FUEL FILTER DRAINING
  IL 212-05-59.pdf 29-Mar-05 MAIN ROTOR DRAG BRACE P/N 204-011-140-ALL
  IL 212-05-58.pdf 14-Feb-05 COLD WEATHER USE OF KEROSENE FUELS FOR 212 AND 412 HELICOPTERS
  IL 212-05-57.pdf 07-Feb-05 CREW SEATS P/N 412-070-810-ALL: NOTIFICATION OF POSSIBLE DAMAGE TO SEAT ATTENUATOR GUIDE PIN P/N 222-620-821-101
  IL 212-04-54 Grip Crack.pdf 13-Jul-04 MAIN ROTOR GRIPS 204-011-121-009, 117 AND 121
  IL 212-00-35.pdf 08-Jun-04 DRAIN MAPS
  IL 212-03-53.pdf 23-Dec-03 P/N 214-070-300-001/-101 INTERNAL RESCUE HOIST CABLE CUTTER AND PYROTECHNIC CARTRIDGE
  IL 212-03-52 .pdf 15-Oct-03 INTER TURBINE TEMPERATURE INDICATORS
  IL 212-03-51.pdf 30-Sep-03 MAIN ROTOR GRIP 204-011-121-005/-009-/-117/-121 ULTRASONIC INSPECTION COURSES
  IL 212-02-50.pdf 10-Dec-02 IMPROVED WIPER MOTORS P/N 204-070-907-103/104
  IL 212-02-49 .pdf 10-Apr-02 204-011-121-009/-121 M/R GRIP ULTRASONIC INSPECTION OF
  IL 212-02-48.pdf 18-Mar-02 204-011-121-009/-121 M/R GRIP ULTRASONIC INSPECTION OF
  IL 212-02-47.pdf 05-Feb-02 204-011-121-009/-121 M/R GRIP ULTRASONIC INSPECTION OF
  IL 212-01-46.pdf 29-Nov-01 STATUS REPORT ON MEDIUM HELICOPTER MAST ASB 212-00-106, REV B
  IL 212-01-45.pdf 03-Aug-01 ENGINE MANUAL FUEL CONTROL OPERATION
  IL 212-01-44.pdf 20-Jun-01 ALL OWNERS/OPERATORS OF BELL 204B, 205, 205B, 212, 412, 412EP, 412CF, AND UH-1H-II HELICOPTERS
  IL 212-01-41.pdf 15-Jun-01 ALL OWNERS/OPERATORS OF BELL 204, 205, 205B, 212, AND UH-1H-II SERIES HELICOPTERS
  IL 212-01-43.pdf 20-Apr-01 TORQUE ON FLIGHT CONTROL BOLTS
  IL 212-01-42.pdf 19-Apr-01 ENGINE ACCESSORY GEARBOX OIL DRAIN VALVE P/N 209-062-010-001, INSTALLATION OF
  IL 212-00-40.pdf 01-Sep-00 STATUS REPORT ON MEDIUM MAST ASB 212-00-106, REV. B
  IL 212-00-39.pdf 18-Aug-00 STATUS REPORT ON MEDIUM MAST ASB
  IL212-00-38A.pdf 08-Aug-00 FEDERAL AVIATION ADMINISTRATION (FAA) AD 2000-15-52 ALTERNATE MEANS OF COMPLIANCE (AMOC) STATEMENT FOR TRUNNIONS 204-011-105-001 AND 204-011-105-103
  IL212-00-37.pdf 03-Aug-00 FAA AIRWORTHINESS DIRECTIVE 2000-15-52
  IL 212-00-36.pdf 02-Jun-00 MAIN ROTOR GRIP 204-011-121-121
  IL 212-00-33.pdf 20-Apr-00 MAIN ROTOR MAST 204-011-450-ALL; INSPECTION AND RETIREMENT INDEX NUMBER (RIN) LIFE REDUCTION
  IL 212-99-31.pdf 23-Sep-99 COMBINING GEARBOX OIL TEMP SWITCH


Additional Information:

For technical questions regarding Bell Helicopter Products, Contact Product Support Engineering.

Send questions, comments, suggestions, or corrections related to this web site to mts-medium@bh.com.